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Aerospace Material Specification (13)

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Aerospace (13)

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Additive manufacturing (12) Manufacturing processes (12) Alloys (7) Metals (6) Production control (6) Chemicals (5) Cobalt alloys (5) Containers (5) Oxygen (5) Gases (4) Hazardous materials (4) Heat treatment (4) Nickel alloys (4) Production (4) Tensile strength (4) Titanium alloys (4) CAD, CAM, and CAE (3) Control systems (3) Identification numbers (3) Powder metallurgy (3) Supply chain management (3) Casting alloys (2) Conductivity (2) Machining processes (2) Materials properties (2) Standardization (2) Coatings, colorants, and finishes (1) Corrosion (1) Corrosion resistant alloys (1) Finishing (1) Lasers (1) Materials handling (1) Metallurgy (1) Parts (1) Suppliers (1) Test procedures (1) Wrought alloys (1)

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AMS AM Additive Manufacturing Metals (13)

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Select Wire Fed Laser Directed Energy Deposition Additive Manufacturing Process (L-DED-wire)

Wire Fed Laser Directed Energy Deposition Additive Manufacturing Process (L-DED-wire)

AMS AM Additive Manufacturing Metals

Aerospace Material Specification
AMS7010
Current

Published 2020-01-14 by SAE International in United States

This specification establishes process controls for the repeatable production of preforms using the wire fed laser directed energy deposition (L-DED-wire) process for additive manufacturing. Preforms are intended to be used to manufacture aerospace parts, but usage is not limited to such applications.

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Select Precipitation Hardenable Steel Alloy, Corrosion and Heat-Resistant Powder for Additive Manufacturing 16.0Cr - 4.0Ni - 4.0Cu - 0.30Nb

Precipitation Hardenable Steel Alloy, Corrosion and Heat-Resistant Powder for Additive Manufacturing 16.0Cr - 4.0Ni - 4.0Cu - 0.30Nb

AMS AM Additive Manufacturing Metals

Aerospace Material Specification
AMS7012
Current

Published 2019-11-14 by SAE International in United States

This specification covers a corrosion and heat-resistant steel alloy in the form of pre-alloyed powder.

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Select Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe

Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe

AMS AM Additive Manufacturing Metals

Aerospace Material Specification
AMS7008
Current

Published 2019-03-26 by SAE International in United States

This specification covers a corrosion and heat-resistant nickel alloy in the form of pre-alloyed powder.

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Select Titanium Alloy, High Temperature Applications, Powder for Additive Manufacturing, Ti - 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo

Titanium Alloy, High Temperature Applications, Powder for Additive Manufacturing, Ti - 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo

AMS AM Additive Manufacturing Metals

Aerospace Material Specification
AMS7014
Current

Published 2019-03-11 by SAE International in United States

This specification covers a heat-resistant titanium alloy in the form of pre-alloyed powder.

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Select Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate Ti-6Al-4V Stress Relieved

Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate Ti-6Al-4V Stress Relieved

AMS AM Additive Manufacturing Metals

Aerospace Material Specification
AMS7004
Current

Published 2019-01-31 by SAE International in United States

This specification covers preforms fabricated up through 5.5 inches (140 mm) inclusive in deposition width thickness (see 8.2.5) using a Plasma Arc Directed Energy Deposition (PA-DED) additive manufacturing process on a Ti-6Al-4V substrate that are subjected to post-deposition stress relief heat treatment. This is a wire fed additive manufacturing process. If required by the CEO, preforms may require subsequent machining to meet requirements for their intended final part application.

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Select Wire Fed Plasma Arc Directed Energy Deposition Additive Manufacturing Process

Wire Fed Plasma Arc Directed Energy Deposition Additive Manufacturing Process

AMS AM Additive Manufacturing Metals

Aerospace Material Specification
AMS7005
Current

Published 2019-01-31 by SAE International in United States

This specification establishes process controls for the repeatable production of preforms by Wire Fed Plasma Arc Directed Energy Deposition (PA-DED). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.

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Select Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 60Ni - 22Cr - 2.0Mo - 14W - 0.35Al - 0.03La

Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 60Ni - 22Cr - 2.0Mo - 14W - 0.35Al - 0.03La

AMS AM Additive Manufacturing Metals

Aerospace Material Specification
AMS7013
Current

Published 2019-01-03 by SAE International in United States

The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 µm) and that no powder (0.0 wt.%) greater than 40 mesh (425 µm) is allowed.

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Select Laser Powder Bed Fusion Process

Laser Powder Bed Fusion Process

AMS AM Additive Manufacturing Metals

Aerospace Material Specification
AMS7003
Current

Published 2018-06-08 by SAE International in United States

This specification establishes process controls for the repeatable production of aerospace parts by Laser Powder Bed Fusion (L-PBF). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.

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Select Process Requirements for Production of Metal Powder Feedstock for Use in Additive Manufacturing of Aerospace Parts

Process Requirements for Production of Metal Powder Feedstock for Use in Additive Manufacturing of Aerospace Parts

AMS AM Additive Manufacturing Metals

Aerospace Material Specification
AMS7002
Current

Published 2018-06-08 by SAE International in United States

This specification is to prescribe process requirements for production of metal powder feedstock for use in additive manufacturing of aerospace parts.

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Select Laser-Powder Bed Fusion (L-PBF) Produced Parts, Nickel Alloy, Corrosion and Heat-Resistant, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb Stress Relieved, Hot Isostatic Pressed and Solution Annealed

Laser-Powder Bed Fusion (L-PBF) Produced Parts, Nickel Alloy, Corrosion and Heat-Resistant, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb Stress Relieved, Hot Isostatic Pressed and Solution Annealed

AMS AM Additive Manufacturing Metals

Aerospace Material Specification
AMS7000
Current

Published 2018-06-08 by SAE International in United States

This specification covers a corrosion and heat-resistant nickel alloy in the form of parts produced by laser-powder bed fusion (L-PBF) that are subjected to post-deposition stress relief (SR), hot isostatic press (HIP) and solution anneal operations. Parts may require subsequent machining or surface finishing to meet specific application requirements.

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